Results of Ground-Based Testing of Passive Heat Protection for Liquid Helium Temperature Spacecraft Devices


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

Resumo

The paper presents the results of thermal vacuum testing of space technology components and instruments using local helium cryo-panels (“shrouds”) in a liquid nitrogen thermal vacuum chamber. A structural description of prototypes and upgraded helium shrouds is given. The results of experimental layouts at the helium temperature level are presented.

Sobre autores

A. Vshivkov

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
Rússia, Krasnoyarsk

A. Delkov

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
Rússia, Krasnoyarsk

A. Kishkin

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
Rússia, Krasnoyarsk

N. Lavrov

Bauman Moscow State Technical University

Autor responsável pela correspondência
Email: lavrovna@bmstu.ru
Rússia, Moscow

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Springer Science+Business Media, LLC, part of Springer Nature, 2019